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[texts]Effect of variation in diameter and pitch of rivets on compressive strength of panels with z-section stiffeners.: I, panels with close stiffener spacing that fail by local buckling - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003638639&ix=nu&I=0&V=D&pm=1
Keywords: Rivets and riveting, Aircraft; Aerodynamics--Research
Downloads: 116
[texts]Determination of the stability and control characteristics of a tailless all-wing airplane model with sweepback in the Langley free-flight tunnel - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003616137&ix=nu&I=0&V=D&pm=1
Keywords: Airplanes, Tailless; Aerodynamics--Research
Downloads: 119
[texts]Charts for the minimum-weight design of 24S-T aluminum-alloy flat compression panels with longitudinal Z-section stiffeners - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003804721&ix=nu&I=0&V=D&pm=1
Keywords: Plates (Engineering; Aerodynamics--Research
Downloads: 276
[texts]On stability and turbulence of fluid flows - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF003764328&ix=nu&I=0&V=D&pm=1
Keywords: Aerodynamics; Turbulence
Downloads: 269
[texts]On the theory of the turbulent boundary layer - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF003778607&ix=nu&I=0&V=D&pm=1
Keywords: Aeronautics; Turbulent boundary layer
Downloads: 118
[texts]Calculation of the shape of a two-dimensional supersonic nozzle in closed form - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF003778681&ix=nu&I=0&V=D&pm=1
Keywords: Aerodynamics; Supersonic nozzles
Downloads: 228
[texts]Elevated-temperature combined stress-rupture plus fatigue strength of waspaloy having having different aging treatments and/or molybedenum contents - Lewis Research Center
http://uf.catalog.fcla.edu/uf.jsp?st=UF003852979&ix=nu&I=0&V=D&pm=1
Keywords: Nickel alloys--Fatigue; Metals--Fatigue
Downloads: 168
[texts]Performance of basic XJ79-GE-1 turbojet engine and its components - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF003852967&ix=nu&I=0&V=D&pm=1
Keywords: Airplanes--Turbojet engines
Downloads: 226
[texts]Transition caused by the Laminar flow separation - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF003778661&ix=nu&I=0&V=D&pm=1
Keywords: Aeronautics; Laminar flow; Boundary layer
Downloads: 83
[texts]Analytical study of shimmy of airplane wheels - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF003779371&ix=nu&I=0&V=D&pm=1
Keywords: Flutter (Aerodynamics; Airplanes--Landing gear
Downloads: 150
[texts]Summary of information on support interference at transonic and supersonic speeds - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003808466&ix=nu&I=0&V=D&pm=1
Keywords: Aerodynamics, Transonic; Aerodynamics, Supersonic
Downloads: 124
[texts]Determination of the stress concentration factor of a stepped shaft stressed in torsion by means of precision strain gages - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF003760230&ix=nu&I=0&V=D&pm=1
Keywords: Aerodynamics; Torsion; Strains and stresses--Research
Downloads: 257
[texts]Research abstracts /National Advisory Committee for Aeronautics (Volume no.86(1955:July18))
http://uf.catalog.fcla.edu/uf.jsp?st=UF001469326
Keywords: Aeronautics Abstracts Periodicals
Downloads: 105
[texts]Airfoil-contour modifications based on [epsilon]-curve method of calculating pressure distribution - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003609112&ix=nu&I=0&V=D&pm=1
Keywords: Aerofoils; Aerodynamics--Research
Downloads: 82
[texts]Some effects of heat transfer at Mach number 2.0 at stagnation temperatures between 2,310° and 3,500° R on a magnesium fin with several leading-edge modifications - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003853254&ix=nu&I=0&V=D&pm=1
Keywords: Heat--Transmission; Aerodynamics--Research; Magnesium--Electrometallurgy
Downloads: 108
[texts]Some examples of the applications of the transonic and supersonic area rules to the prediction of wave drag - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003809079&ix=nu&I=0&V=D&pm=1
Keywords: Aerodynamics, Transonic; Aerodynamics, Supersonic; Aerodynamics--Research
Downloads: 230
[texts]Lecture series "boundary layer theory.": Part II, turbulent flows - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF003780859&ix=nu&I=0&V=D&pm=1
Keywords: Aerodynamics; Turbulence; Laminar boundary layer
Downloads: 352
[texts]Index of NACA technical publications (Volume 1915-1949) - United States: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF030392191&ix=pm&I=0&V=D&pm=1
Keywords: Aeronautics--Abstracts
Downloads: 634
[texts]Calculation of stick forces for an elevator with a spring tab - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003613059&ix=nu&I=0&V=D&pm=1
Keywords: Elevators (Airplanes; Aerodynamics--Research
Downloads: 149
[texts]On the turbulent friction layer for rising pressure - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF003779898&ix=nu&I=0&V=D&pm=1
Keywords: Aerodynamics; Laminar boundary layer
Downloads: 209
[texts]Research abstracts /National Advisory Committee for Aeronautics (Volume no.40(1953:Mar.27))
http://uf.catalog.fcla.edu/uf.jsp?st=UF001469326
Keywords: Aeronautics Abstracts Periodicals
Downloads: 105
[texts]Aerodynamic characteristics of the NACA 747A315 and 747A415 airfoils from tests in the NACA two-dimensional low-turbulence pressure tunnel - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003638506%26ix=nu%26I=0%26V=D%26pm=1
Keywords: Mach number; Aerofoils; Drag (Aerodynamics; Lift (Aerodynamics; Aerodynamics--Research; Aerodynamics--Research
Downloads: 626
[texts]Aircraft configurations developing high lift-drag ratios at high supersonic speeds - Ames Research Center
http://uf.catalog.fcla.edu/uf.jsp?st=UF003809137&ix=nu&I=0&V=D&pm=1
Keywords: Drag (Aerodynamics; Aerodynamics, Supersonic; Aerodynamics--Research
Downloads: 251
[texts]Index of NACA technical publications (Volume 1949-May 1951) - United States: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF030392191&ix=pm&I=0&V=D&pm=1
Keywords: Aeronautics--Abstracts
Downloads: 292
[texts]Wind-tunnel investigation of a rectangular NACA 2212 airfoil with semispan ailerons and with nonperforated, balanced double split flaps for use as aerodynamic brakes - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003614467&ix=nu&I=0&V=D&pm=1
Keywords: Flaps (Airplanes; Airplanes--Wings--Testing; Aerodynamics--Research
Downloads: 303
[texts]Research abstracts /National Advisory Committee for Aeronautics (Volume no.69(1954:Sept.7))
http://uf.catalog.fcla.edu/uf.jsp?st=UF001469326
Keywords: Aeronautics Abstracts Periodicals
Downloads: 102
[texts]Monthly list of documents released by the NACA during .. (Volume 270(1949:Sept.)) - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF030954133&ix=pm&I=0&V=D&pm=1
Keywords: Aeronautics
Downloads: 41
[texts]On the design of airfoils in which the transition of the boundary layer is delayed - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF003778659&ix=nu&I=0&V=D&pm=1
Keywords: Aerodynamics; Laminar flow; Aerofoils
Downloads: 149
[texts]Approximate method for estimating the incompressible laminar boundary-layer characteristics on a flat plate in slipping flow - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003810747&ix=nu&I=0&V=D&pm=1
Keywords: Laminar boundary layer; Aerodynamics--Research
Downloads: 94
[texts]Monthly list of documents released by the NACA during .. (Volume 274(1950:Jan.)) - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF030954133&ix=pm&I=0&V=D&pm=1
Keywords: Aeronautics
Downloads: 38
[texts]Research abstracts /National Advisory Committee for Aeronautics (Volume no.56(1954:Jan13))
http://uf.catalog.fcla.edu/uf.jsp?st=UF001469326
Keywords: Aeronautics Abstracts Periodicals
Downloads: 113
[texts]Electromagnetic-analogy method of solving lifting-surface-theory problems - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003613188&ix=nu&I=0&V=D&pm=1
Keywords: Compressibility; Aerodynamics--Research
Downloads: 136
[texts]Tire friction coefficients and their relation to ground-run distance in landing - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003808568&ix=nu&I=0&V=D&pm=1
Keywords: Airplanes--Tires--Traction; Aerodynamics--Research
Downloads: 227
[texts]Tensile tests of NACA and conventional machine-countersunk flush rivets - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003807455&ix=nu&I=0&V=D&pm=1
Keywords: Rivets and riveting, Aircraft; Aerodynamics--Research
Downloads: 188
[texts]Flight investigation at high mach numbers of several methods of measuring static pressure on an airplane wing - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003613532&ix=nu&I=0&V=D&pm=1
Keywords: Mach number; Bombers; Aerodynamics--Research
Downloads: 119
[texts]Lifting-surface-theory values of the damping in roll and of the parameter used in estimating aileron stick forces - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003614499&ix=nu&I=0&V=D&pm=1
Keywords: Ailerons; Damping (Mechanics; Aerodynamics--Research
Downloads: 93
[texts]Research abstracts /National Advisory Committee for Aeronautics (Volume no.71(1954:Oct.7))
http://uf.catalog.fcla.edu/uf.jsp?st=UF001469326
Keywords: Aeronautics Abstracts Periodicals
Downloads: 87
[texts]Research abstracts /National Advisory Committee for Aeronautics (Volume no.70(1954:Sept.21))
http://uf.catalog.fcla.edu/uf.jsp?st=UF001469326
Keywords: Aeronautics Abstracts Periodicals
Downloads: 74
[texts]Numerical evaluation of the [epsilon]-integral occurring in the Theodorsen arbitrary-airfoil potential theory - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003605363&ix=nu&I=0&V=D&pm=1
Keywords: Conformal mapping; Harmonic analysis; Aeronautics--Research
Downloads: 93
[texts]Heat transmission in the boundary layer - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF003759949&ix=nu&I=0&V=D&pm=1
Keywords: Aerodynamics; Turbulent boundary layer
Downloads: 119
[texts]General characteristics of the flow through nozzles at near critical speeds - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF003780314&ix=nu&I=0&V=D&pm=1
Keywords: Aerodynamics; Supersonic nozzles--Research
Downloads: 249
[texts]Research abstracts /National Advisory Committee for Aeronautics (Volume no.80(1955:Mar.29))
http://uf.catalog.fcla.edu/uf.jsp?st=UF001469326
Keywords: Aeronautics Abstracts Periodicals
Downloads: 105
[texts]Temperature recovery factors on a slender 12° cone-cylinder at Mach numbers from 3.0 to 6.3 and angles of attack up to 45° - Ames Research Center
http://uf.catalog.fcla.edu/uf.jsp?st=UF003854733&ix=nu&I=0&V=D&pm=1
Keywords: Heat--Transmission; Laminar boundary layer--Research; Aerodynamics--Research
Downloads: 102
[texts]Nonlinear theory of a hot-wire anemometer - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF003778597&ix=nu&I=0&V=D&pm=1
Keywords: Airplanes--Wings; Hot-wire anemometer
Downloads: 126
[texts]Automatically variable control linkage and its effect on the lateral-control characteristics of a high-speed fighter airplane - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003666890&ix=nu&I=0&V=D&pm=1
Keywords: Fighter planes; Ailerons; Aerodynamics
Downloads: 116
[texts]Supersonic-tunnel tests of projectiles in Germany and Italy - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003598987&ix=nu&I=0&V=D&pm=1
Keywords: Mach number; Projectiles, Aerial; Aerodynamics--Research
Downloads: 150
[texts]Pressure distributions on three bodies of revolution to determine the effect of Reynolds number up to and including the transonic speed range

Keywords: Body of revolution; Aerodynamics, Transonic
Downloads: 116
[texts]Flat plate cascades at supersonic speed - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF003807842&ix=nu&I=0&V=D&pm=1
Keywords: Cascades (Fluid dynamics; Aerodynamics--Research
Downloads: 92
[texts]Experimental verification of the rudder-free stability theory for an airplane model equipped with rudders having negative floating tendency and negligible friction - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003806635&ix=nu&I=0&V=D&pm=1
Keywords: Elevators (Airplanes; Aerodynamics--Research
Downloads: 134
[texts]Effect of the lift coefficient on propeller flutter - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003804948&ix=nu&I=0&V=D&pm=1
Keywords: Oscillating wings (Aerodynamics; Propellers--Research
Downloads: 118
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